WESTLAND WALLACE

WESTLAND WALLACE - Light bomber and army co-operation biplane derived from Wapiti, with split-axle undercarriage and Bristol Pegasus engine. Private venture prototype (Westland P.V.6) first flown October 31, 1931, leading to adoption by RAF. To Specification 19/32, 57 Wapiti IIA airframes (mostly in store, and unflown) converted to Westland Wallace I, as well as two Westland prototype and development aircraft; eight more built as new. Then to Specification G.31/35, the RAF bought 107 Westland Wallace Us (including three Wapiti conversions) differing principally in having a totally enclosed canopy over the two cockpits, with a revised mounting for the Lewis gun in the rear cockpit. Westland Wallace I had 550 hp Bristol Pegasus II engine, replaced by supercharged 665 hp Pegasus IV in Westland Wallace II, with larger diameter propeller. Westland Wallaces were used to equip RAF Special Reserve and, later, AAF squadrons in UK, starting with No/501 (City of Bristol) in January 1933. In September 1939, some 125 Westland Wallaces were still on strength (41 of them Mk Is). They flew on until mid-1943, serving as trainers at Bombing and Gunnery Schools, and in other support roles including target-towing. Data for Westland Wallace II:
Max speed, 158 mph (254 kmlh) at 15,000ft (4,572 m). Gross weight, 5,750 Ib (2,608 kg). Span, 46 ft 5 in (14.14m). Length, 34 ft 2 in (10.41 m).